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The significance of coherent flow structures for the turbulent mixing ...

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6.1 Experimental set-up<br />

<strong>the</strong> (virtual) slave cameras 1 and 2, located behind <strong>the</strong> mirrors, are not presented in <strong>the</strong> table<br />

as <strong>the</strong>se can be considered as identical with <strong>the</strong> corresponding master cameras 3 and 4.<br />

y<br />

x<br />

main <strong>flow</strong>-direction<br />

c<br />

a<br />

10 wall-units light-sheet separation<br />

~94°<br />

b<br />

8<br />

7<br />

6<br />

5<br />

4<br />

2<br />

1<br />

3<br />

FIGURE 6.2: Experimental set-up <strong>for</strong> ÚQ -investigation. 1-4 digital cameras, 5 lens, 6 mirror, 7 polarising<br />

beam-splitter cube, 8 absorbing material.<br />

camera á [mm] Ä [mm] OP [mm] R [deg]<br />

3 628 -573 850 47.1<br />

4 -608 -565 829 47.6<br />

TABLE 6.1: Camera position, observation<br />

distances and viewing angles with respect<br />

to <strong>the</strong> centre <strong>of</strong> <strong>the</strong> field <strong>of</strong> view.<br />

For magnification and field <strong>of</strong> view adjustments each Scheimpflug-adapter was mounted<br />

on a two-axis micrometer translation stage, and <strong>the</strong> polarising beam splitter-cubes and mirrors<br />

in front <strong>of</strong> <strong>the</strong> lenses were connected to two-axis tilt-rotation stages and gimbal mirror mounts.<br />

To obtain ideal particle images <strong>for</strong> <strong>the</strong> image analysis algorithms ÓöÎ<br />

(bright circles, pixel in<br />

diameter, surrounded by a dark background), <strong>the</strong> imaging <strong>of</strong> <strong>the</strong> field <strong>of</strong> view was per<strong>for</strong>med<br />

by means <strong>of</strong> 100 mm Carl Zeiss lenses with an aperture <strong>of</strong> 8. This leads to a complete erasure<br />

<strong>of</strong> all optical aberrations and out-<strong>of</strong>-focus effects. <strong>The</strong> arrangement was installed<br />

<br />

below<br />

<strong>the</strong> wind-tunnel, as shown in figure 6.2. <strong>The</strong> mean observation S<br />

distance was mm and<br />

*:U<br />

<strong>the</strong><br />

opening angle between <strong>the</strong> left and right camera systems was T set to to resolve <strong>the</strong> out-<strong>of</strong>plane<br />

motion with sufficient accuracy according to figure 3.5. This is important because <strong>the</strong><br />

out-<strong>of</strong>-plane component is required to calculate <strong>the</strong> dominant Reynolds shear-stress component<br />

V turb W<br />

glued on an aluminium plate and attached with a micrometer translation stage in such a way<br />

that a parallel motion <strong>of</strong> <strong>the</strong> grid could be achieved in vertical direction. This grid was aligned<br />

with each light-sheet one after ano<strong>the</strong>r and recorded each time with <strong>the</strong> four cameras (be<strong>for</strong>e<br />

and after <strong>the</strong> experiment in order to pro<strong>of</strong> <strong>the</strong> conservation <strong>of</strong> <strong>the</strong> boundary conditions during<br />

<strong>the</strong> experiment). As any horizontal translation <strong>of</strong> <strong>the</strong> target could be excluded with this device,<br />

Î& 6(7 . For <strong>the</strong> calibration <strong>of</strong> <strong>the</strong> system a regular grid with Ó mm line spacing was<br />

99

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